MIL-W-5088 Revision L:1991
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
Available format(s)
PDF
Superseded date
01-04-1998
Published date
10-05-1991
Publisher
Covers aspects from selection to the installation of wiring and wiring devices used in aerospace vehicles, including helicopters, airplanes, lighter-than-air vehicles, and missiles. Coverage includes application, applicable documents, terminology interpretation, deviations, materials, metals, nonmetals, sealing materials, maintenance considerations, ambient temperature, and missile wiring application.
This specification covers all aspects from the selection through installation of wiring and wiring devices used in aerospace vehicles.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN
|
| DocumentType |
Standard
|
| Pages |
88
|
| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Superseded
|
| SupersededBy |
| MIL-R-85895 Base Document:1988 | RACK, BOMB EJECTOR, AIRCRAFT BRU-32/A |
| MIL-C-6781 Revision B:1960 | CONTROL PANEL, AIRCRAFT EQUIPMENT, RACK OR CONSOLE MOUNTED |
| DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| MIL-R-83372 Base Document:1972 | RELAY, ELECTROMAGNETIC, HYBRID, EMI SUPPRESSED, GENERAL SPECIFICATION FOR |
| MIL-I-83294 Base Document:1971 | INSTALLATION REQUIREMENT, AIRCRAFT PROPULSION SYSTEMS, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-R-29583 Base Document:1992 | RADIO SET |
| MIL S 24317 : 0 | SWITCH, MULTI-STATION, PUSHBUTTON (ILLUMINATED AND NON-ILLUMINATED), GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-E-23001 Revision B:1976 | ELECTRIC GENERATING SYSTEM, VARIABLE SPEED CONSTANT FREQUENCY, AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL I 7627 : F | INDICATOR, TURN AND SLIP 28V DC |
| MIL-L-6503 Revision H:1975 | LIGHTING EQUIPMENT, AIRCRAFT, GENERAL SPECIFICATION FOR INSTALLATION OF |
| DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL-A-22145 Revision C:1992 | ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
| DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-I-85071 Revision A:1992 | INVERTERS, AIRCRAFT, DC TO AC, GENERAL SPECIFICATION FOR |
| MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
| MIL-HDBK-83575 Base Document:1998 | GENERAL HANDBOOK FOR SPACE VEHICLE WIRING HARNESS DESIGN AND TESTING |
| MIL-T-81714 Revision E:1988 | TERMINAL JUNCTION SYSTEM (TJS), ENVIRONMENT RESISTANT GENERAL SPECIFICATION FOR |
| MIL-C-7135 Revision F:1967 | Compressor, Pneumatic, 3,000 PSI -- 2 SCFM Aero 2A (*), Aero 2A-1 (*), Aero 2B (*), and Aero 2B-1 (*) |
| MIL-R-81046 Base Document:1964 | RECORDER-REPRODUCER SET, SOUND AN/AQH-1(V) |
| MIL-C-23697 Base Document:1963 | COMPUTER SET, NAVIGATIONAL AN/ASN-42(*) |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/6(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-HDBK-1587 Base Document:1996 | MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM |
| DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-81973 Base Document:1974 | AIRCREW AUTOMATED ESCAPE SYSTEMS, TEST VEHICLES FOR GROUND TRACK PERFORMANCE TESTING, ROCKET AND/OR JET ENGINE PROPELLED; GENERAL SPECIFICATION FOR |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL T 28800 : E | TEST EQUIPMENT FOR USE WITH ELECTRICAL AND ELECTRONIC EQUIPMENT GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-R-81876 Revision B:1988 | RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
| MIL W 8777 : C | WIRE, ELECTRICAL, SILICONE-INSULATED COPPER 600-VOLT, 200 DEGREE C |
| DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT |
| DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| DEFSTAN 00-69(PT2)/1(1998) : 1998 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM - PART 2: DESIGN PRINCIPLES AND PRACTICES FOR, AND GUIDE TO, THE IMPLEMENTATION OF THE AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| MIL-H-8891 Revision A:1978 | HYDRAULIC SYSTEMS, MANNED FLIGHT VEHICLES TYPE 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-J-23013 Base Document:1961 | JUNCTION BOX JEU-25 (*)/A |
| DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| MIL-E-45782 Revision C:1993 | ELECTRICAL WIRING, PROCEDURES FOR |
| MIL-A-81621 Base Document:1969 | ACCELEROMETER, ELECTRICAL, LINEAR ABU-13/A |
| MIL-DTL-8777 Revision F:2011 | WIRE, ELECTRICAL, SILICONE-INSULATED, COPPER, 600-VOLT, 200 DEGREES C |
| MIL-A-26624 Revision B:1981 | AIR CONDITIONER, A/M32C-5, TRAILER MOUNTED, VAPOR CYCLE, ELECTRIC MOTOR DRIVEN |
| MIL-M-25047 Revision C:1968 | MARKINGS AND EXTERIOR FINISH COLORS FOR AIRPLANES, AIRPLANE PARTS, AND MISSILES (BALLISTIC MISSILES EXCLUDED) |
| MIL-I-85671 Base Document:1987 | INDICATOR, FREQUENCY CHANNEL ID-2121A/ARC, ID-2229A/ARC AND ID-2303/ARC |
| MIL-D-81358 Revision B:1970 | DISPLAY GROUP, TACTICAL DATA AN/ASA-66 |
| MIL-T-23733 Revision A:1968 | TRANSMITTER, RATE GYROSCOPE T-751 (/AJB-3) |
| MIL-A-23670 Revision A:1965 | ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-50(*) |
| MIL M 87158 : A | MANUALS, TECHNICAL, AIRCRAFT BATTLE DAMAGE ASSESSMENT AND REPAIR |
| MIL-B-81365 Base Document:1966 | BLEED AIR SYSTEMS, GENERAL SPECIFICATIONS FOR |
| MIL-C-22764 Revision C:1964 | CODER RECEIVER TRANSMITTER K & Y532A ASQ |
| MIL-S-8512 Revision D:1974 | SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
| MIL-S-5594 Revision B:1971 | SWITCH, TOGGLE, ELECTRICALLY HELD SEALED GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL B 8075 : D | BRAKE CONTROL SYSTEMS, ANTI SKID, AIRCRAFT WHEELS, INSTRUCTIONS FOR PREPARATION OF |
| MIL-S-83129 Revision A:1972 | SPECTROMETER, FLUID ANALYSIS A/E35U-3 |
| DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
| SAE AS 8700 : 1999 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
| MIL-M-9397 Revision E:1979 | FREQUENCY CONVERTER, MOBILE, TYPE MC-1A |
| MIL-S-8812 Revision D:1975 | STEERING SYSTEM, AIRCRAFT GENERAL REQUIREMENTS FOR |
| MIL-S-8710 Revision B:1969 | STRAINER, AIRFRAME FUEL SYSTEM, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
| MIL S 8805/48 : F | SWITCH, SENSITIVE, ROLLER LEVER, SELF RETURN, RESILIENT SEAL, FLUID RESISTANT |
| SAE AIR 5271 : 2009 | A GUIDELINE FOR APPLICATION OF HIGH-DENSITY FIBER OPTIC INTERCONNECTS TO AEROSPACE PLATFORMS |
| MIL-E-7016 Revision F:1976 | ELECTRIC LOAD AND POWER SOURCE CAPACITY, AIRCRAFT ANALYSIS OF |
| MIL-R-21073 Revision A:1960 | RECORDER, MAGNETIC DISTORTION, RO-32/ASQ |
| DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL F 26685 : B NOTICE 1 | FLIGHT DIRECTOR SYSTEM, DESIGN AND INSTALLATION OF |
| MIL-DTL-26126 Revision C:2002 | RELAYS, ELECTRICAL, OVERVOLTAGE, DC, GENERAL SPECIFICATION FOR |
| MIL-A-23887 Revision A:1965 | ALTIMETER SET, ELECTRONIC AN/APN-141 (V) |
| MIL-C-85518 Base Document:1984 | COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
| MIL-D-23222 Revision A:1971 | DEMONSTRATION REQUIREMENTS FOR HELICOPTERS |
| MIL-I-8673 Base Document:1955 | INSTALLATION AND TEST OF AIRCRAFT FLEXIBLE WEAPONS SYSTEMS |
| MIL-D-81641 Base Document:1972 | DISPLAY, HEAD UP, GENERAL SPECIFICATION FOR |
| MIL-I-81454 Base Document:1967 | INDICATOR, GYROSCOPE, VERTICAL REFERENCE ID-1481 (*)/A |
| MIL-A-81359 Base Document:1970 | AIRCRAFT WEAPONS RELEASE SET AN/AWE-1 |
| MIL-C-19941 Revision A:1966 | CONTROLLER, S-2 COMPASS, TYPE |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| MIL-D-8804 Revision B:1993 | DE-ICING SYSTEM, PNEUMATIC BOOT, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL C 5898 : D | CORD, ELECTRICAL [WF 5/U, WF 14/U,WD 34/U, WM 53/U, WM 85/U] |
| MIL R 26895 : 0 | RELAY, FIELD CONTROL, GENERATOR 28 VOLT DC, TYPE MD AND 1 |
| MIL I 18373 : B | INSTRUMENT AND NAVIGATION EQUIPMENT, AIRCRAFT, INSTALLATION OF |
| MIL-C-85248 Revision A:1984 | CAMERA, STILL PICTURE, PANORAMIC, KA-99A |
| MIL-R-24011 Revision A:1965 | RADAR ALTIMETER WARNING SET AN APQ 107 (*) |
| MIL-R-6463 Revision A:1952 | RELAY, GENERATOR EQUALIZER BUS, TYPE A1 |
| MIL-C-18277 Revision B:1961 | COUPLER, ANTENNA CU-351/AR AND COUPLER, ANTENNA CU-509/AR |
| MIL-C-85642 Base Document:1985 | COMMUNICATIONS CENTRAL AN/ASC-26 |
| MIL C 81125 : NOTICE 1 | COUPLER, ANTENNA CU-1304 (*)/ARC AND MOUNTING MT-3261 (*)/ARC |
| MIL-A-22424 Revision A:1967 | ADAPTERS, COMPENSATING, MS281O7, MA-1 COMPASS SYSTEM |
| DOD-STD-863 Revision B:1979 | WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-5238 Revision C:1974 | PUMP, CENTRIFUGAL, FUEL BOOSTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| SAE ARP 1897 : 2013 | CLAMP SELECTION AND INSTALLATION GUIDE |
| SAE AIR 5575 : 2017 | HOT STAMP WIRE MARKING CONCERNS FOR AEROSPACE VEHICLE APPLICATIONS |
| MIL-G-81665 Base Document:1971 | GENERATOR TRANSMITTER GROUP AN/ASA-76 (U) |
| MIL-A-23622 Base Document:1963 | ACTUATOR, AIRCRAFT, ELECTRO-MECHANICAL, LINEAR, DIRECT CURRENT |
| MIL-STD-681 Revision F:2012 | IDENTIFICATION CODING AND APPLICATION OF HOOKUP AND LEAD WIRE |
| MIL-R-28894 Base Document:1986 | RELAY, HYBRID OR SOLID STATE, SENSORS, ESTABLISHED RELIABILITY GENERAL SPECIFICATION FOR |
| MIL S 8805/43 : G | SWITCH, SENSITIVE, PLUNGER, 7 AMPERES RESILIENT SEAL, FLUID RESISTANT |
| MIL-A-19939 Revision A:1966 | AMPLIFIER, TWO CHANNEL, INTEGRAL, S-2 COMPASS |
| MIL-W-22759 Revision E:1990 | WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY |
| MIL-C-81991 Base Document:1975 | CONVERTER, AIRCRAFT DC TO DC, BOOST GENERAL SPECIFICATION FOR |
| MIL R 26126 : B | RELAY, ELECTRICAL, OVERVOLTAGE DC, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-I-23366 Revision B:1987 | INDICATOR, HORIZONTAL SITUATION ID-1O13(*)/A |
| DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
| MIL-DTL-25561 Revision B:1995 | GRIP ASSEMBLY, CONTROLLER, AIRCRAFT, TYPE MC-2 |
| MIL-R-9221 Base Document:1953 | RELAY, FIELD CONTROL, GENERATOR 24 VOLT DC TYPE M AND 2 |
| MIL-E-85583 Revision A:1987 | ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-G-83380 Base Document:1979 | GENERATOR SET, GAS TURBINE ENGINE DRIVEN, 30 AND 60 KW, 400 HZ |
| MIL-E-25499 Revision C:1970 | ELECTRICAL SYSTEMS, AIRCRAFT, DESIGN AND INSTALLATION OF, GENERAL REQUIREMENTS FOR |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| MIL-F-23447 Base Document:1962 | FIRE WARNING SYSTEMS, AIRCRAFT, RADIATION SENSING TYPE, TEST AND INSTALLATION OF |
| DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
| MIL-W-26217 Revision B:1985 | WINCH, DRUM, POWER OPERATED AF E24H 1, CARGO LOADING, 4OOO POUND CAPACITY, VARIABLE SPEED, 28V DC PORTABLE |
| MIL-N-81207 Revision A:1973 | NAVIGATIONAL SET, TACAN AN/ARN-84 (V) |
| SAE AS 55941 : 2013 | SWITCHES, TOGGLE, ELECTRICALLY HELD, SEALED, GENERAL SPECIFICATION FOR |
| SAE ARP 1070E : 2019 | DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
| SAE ARP 1070 : 2014 | DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY |
| MIL-G-23081 Revision C:1972 | GYROSCOPE INDICATOR SYSTEM VERTICAL. |
| MIL-D-19326 Revision H:1990 | DESIGN AND INSTALLATION OF LIQUID OXYGEN SYSTEMS IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-R-81498 Revision C:1979 | RECEIVING-DECODING GROUP AN/ARA-63 |
| MIL-G-23083 Revision C:1972 | GYROSCOPE, RATE SWITCHING MS 17399 |
| MIL-B-23431 Revision B:1993 | BEACON, RADAR AN/APN-154(V) |
| MIL-F-8615 Revision D:1976 | FUEL SYSTEM COMPONENTS, GENERAL SPECIFICATION FOR [ASG] |
| MIL-I-85112 Base Document:1978 | INDICATOR SET, VERTICAL SCALE |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-A-85672 Base Document:1987 | AMPLIFIER, RADIO FREQUENCY AM-7177A/ARC |
| MIL-W-18326 Revision A:1956 | WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR |
| MIL-A-81605 Revision D:1984 | ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
| SAE AS 22145 : 2012 | ACCELEROMETER GROUP, COUNTING (MS25447 AND MS25448) |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| MIL-I-81453 Revision A:1977 | INTERROGATOR SET AN APX 76B(V) |
| MIL-T-85678 Base Document:1974 | TRANSPONDER, RADAR TRACKING |
| MIL-A-81296 Revision D:1985 | ALTIMETER SET, ELECTRONIC AN/APN-171(V) |
| MIL M 4803 : D | MOTOR-GENERATOR, 400 HZ PRECISE OUTPUT, GENERAL REQUIREMENTS FOR |
| MIL-L-85314 Revision A:1983 | LIGHT SYSTEMS, AIRCRAFT, ANTI COLLISION, STROBE, GENERAL SPECIFICATION FOR |
| MIL-A-81423 Base Document:1966 | ATTITUDE HEADING REFERENCE SYSTEM AN/ASN-73 |
| MIL D 83753 : NOTICE 2 | DISPENSER, BOMB, TYPE SUU-21/A |
| MIL-I-8672 Revision B:1969 | INSTALLATION AND TEST OF AIRCRAFT PYROTECHNIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR [ASG] |
| MIL-C-85392 Base Document:1987 | CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-7D, GENERAL SPECIFICATION FOR |
| MIL C 7115 : F | CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-C-81883 Base Document:1976 | CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
| MIL-I-7802 Revision A:1967 | INDICATOR, MS 28088, TURN AND SLIP [THREE PHASE] |
| MIL-C-85283 Revision B:1994 | CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW-9 |
| MIL-L-5667 Revision B:1964 | LIGHTING EQUIPMENT, AIRCRAFT INSTRUMENT PANEL, GENERAL SPECIFICATION FOR INSTALLATION OF [ASG] |
| MIL M 23888 : NOTICE 1 | MONITOR, RADIO FREQUENCY ID AND 9O2A/AR |
| MIL S 9419 : E | SWITCH, TOGGLE, MOMENTARY, FOUR-POSITION ON, CENTER OFF, GENERAL SPECIFICATION FOR |
| MIL-C-85373 Revision A:1987 | CONTROL MONITOR SET, GUIDED WEAPON, AN/AWW 12A |
| MIL-T-81821 Base Document:1969 | TRAINERS, MAINTENANCE, EQUIPMENT AND SERVICES GENERAL SPECIFICATION FOR |
| MIL-D-5025 Revision C:1961 | DIRECTION FINDER GROUPS AN/APA-69A AND AN/APA 69C |
| MIL-C-18244 Revision A:1962 | CONTROL AND STABILIZATION SYSTEMS, AUTOMATIC, PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-P-18987 Revision A:1962 | PLOTTING BOARD, TACTICAL DISPLAY PT-396/AS |
| MIL-P-19461 Revision A:1959 | PLOTTING BOARD, TACTICAL DISPLAY, PT-429/A |
| MIL-I-3190 Revision F:1991 | INSULATION SLEEVING, ELECTRICAL, FLEXIBLE, COATED, GENERAL SPECIFICATION FOR |
| MIL-M-24041 Revision C:1981 | MOLDING AND POTTING COMPOUND |
| ASME Y32.2 : LATEST | DRAW AND TERM - GRAPHICS SYMBOLS STANDARDS - FOR ELECTRICAL AND ELECTRONIC DIAGRAMS |
| MS33540 Revision J:1986 | SAFETY WIRING AND COTTER PINNING, GENERAL PRACTICES FOR |
| MIL-S-23190 Revision E:1986 | STRAPS, CLAMPS AND MOUNTING HARDWARE, PLASTIC FOR CABLE HARNESS TYING AND SUPPORT |
| MIL-W-22759 Revision E:1990 | WIRE, ELECTRIC, FLUOROPOLYMER-INSULATED, COPPER OR COPPER ALLOY |
| MIL C 22520 : F | CRIMPING TOOLS, TERMINAL HAND OR POWER ACTUATED, WIRE TERMINATION AND TOOL KITS - GENERAL SPECIFICATION FOR |
| MS27212 Revision P:1994 | TERMINAL BOARD, ASSEMBLY, MOLDED IN STUD, ELECTRIC |
| MS25281 Revision K:1978 | CLAMP, LOOP PLASTIC, WIRE SUPPORT |
| MS90387 Revision H:2007 | TOOL, HAND, ADJUSTABLE FOR PLASTIC AND METAL TIEDOWN STRAPS |
| MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
| MIL-STD-970 Base Document:1987 | STANDARDS AND SPECIFICATIONS, ORDER OF PREFERENCE FOR THE SELECTION OF |
| MIL-C-7762 Revision A:1967 | COMPASS, INSTALLATION OF |
| MIL C 83517 : 0 | CONNECTOR, COAXIAL, RADIO FREQUENCY FOR COAXIAL, STRIP OR MICROSTRIP TRANSMISSION LINE, GENERAL SPECIFICATION FOR |
| MIL A 55339 : A | ADAPTER, CONNECTOR, COAXIAL, RADIO FREQUENCY, (BETWEEN SERIES & WITHIN SERIES) GENERAL SPECIFICATION FOR |
| DOD STD 100 : C NOTICE 6 | ENGINEERING DRAWING PRACTICES |
| MS25439 Revision A:1964 | SPLICE PERMANENT CRIMP STYLE, 2 WAY TYPE FOR ALUMINUM AIRCRAFT WIRE CLASS 1, |
| MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
| MS25440 Revision C:1974 | WASHER FOR USE WITH AIRCRAFT ALUMINUM TERMINALS |
| MIL-STD-1353 Revision C:2014 | ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF |
| DOD-STD-863 Revision B:1979 | WIRING DATA AND SYSTEM SCHEMATIC DIAGRAMS PREPARATION OF |
| MS25436 Revision A:1964 | TERMINAL, LUG, CRIMP STYLE 90 DEGREES UPRIGHT TYPE, FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 |
| MS25274 Revision G:1982 | CAP, ELECTRICAL, (WIRE END, CRIMP STYLE, TYPE 2, CLASS 1) FOR 105 DEGREE C TOTAL CONDUCTOR TEMPERATURE |
| MIL-T-81490 Revision A:1991 | TRANSMISSION LINES, TRANSVERSE ELECTROMAGNETIC MODE |
| MIL-T-7099 Revision E:1979 | TERMINAL, LUG AND SPLICE, CRIMP STYLE ALUMINUM FOR ALUMINUM AIRCRAFT WIRE |
| MIL-C-26637 Revision A:1987 | CONNECTORS, COAXIAL, RADIO FREQUENCY, SERIES LT |
| MIL C 3650 : A | CONNECTOR, COAXIAL, RADIO FREQUENCY, SERIES LC |
| MIL-T-81714 Revision E:1988 | TERMINAL JUNCTION SYSTEM (TJS), ENVIRONMENT RESISTANT GENERAL SPECIFICATION FOR |
| MIL-STD-889 Revision C:2016 | DISSIMILAR METALS |
| MS21919 Revision E:1981 | CLAMP, LOOP TYPE, CUSHIONED, SUPPORT |
| MIL-C-85049 Revision A:1990 | CONNECTOR ACCESSORIES, ELECTRICAL GENERAL SPECIFICATION FOR |
| MIL-T-43435 Revision B:1974 | TAPE, LACING, AND TYING |
| MIL-M-81260 Revision A:1971 | MANUALS, TECHNICAL, AIRCRAFT/SYSTEM/EQUIPMENT MAINTENANCE |
| MIL-C-85485 Revision A:1983 | CABLE, ELECTRIC, FILTER LINE, RADIO FREQUENCY ABSORPTIVE |
| MIL C 39012 : C | GENERAL SPECIFICATION FOR RADIO FREQUENCY COAXIAL CONNECTORS |
| MIL-HDBK-216 Base Document:1962 | R.F. Transmission Lines and Fittings (Future Acquisitions may refer to EIA-979) |
| MS21266 Revision E:1981 | GROMMET PLASTIC EDGING |
| MIL-STD-1388-1 Revision A:1983 | LOGISTIC SUPPORT ANALYSIS |
| MIL S 8516 : F | SEALING COMPOUND, POLYSULFIDE RUBBER, ELECTRIC CONNECTORS AND ELECTRICAL SYSTEMS CHEMICALLY CURED |
| MIL C 25516 : D | CONNECTOR, ELECTRICAL, MINIATURE, COAXIAL, ENVIRONMENT RESISTANT TYPE, GENERAL SPECIFICATION FOR |
| MIL-I-23594 Revision C:1988 | INSULATION TAPE, ELECTRICAL, HIGH TEMPERATURE, POLYTETRAFLUOROETHYLENE, PRESSURE SENSITIVE |
| MIL-T-81714-12 Revision C:1988 | TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, WIRE IN-LINE JUNCTIONS, DOUBLE, SERIES 1 |
| MIL I 23053 : D | INSULATION SLEEVING, ELECTRICAL, HEAT SHRINKABLE MODIFIED FLUOROPOLYMER, CROSSLINKED |
| MIL-B-7883 Revision B:1968 | BRAZING OF STEELS, COPPER, COPPER ALLOYS, NICKEL ALLOYS, ALUMINUM AND ALUMINUM ALLOYS |
| MIL C 3643 : A | CONNECTOR, COAXIAL RADIO FREQUENCY, SERIES HN ASSOCIATED FITTINGS GENERAL SPECIFICATION FOR |
| MIL-C-39029 Revision D:1988 | CONTACT, ELECTRICAL CONNECTOR, GENERAL SPECIFICATION FOR |
| MIL S 23586 : E | SEALING COMPOUND, ELECTRICAL, SILICONE RUBBER, ACCELERATOR REQUIRED |
| MS90376 Revision E:1993 | CAP, DUST, PLASTIC, ELECTRIC CONNECTOR |
| MS35489 Revision K:2012 | GROMMETS, SYNTHETIC AND SILICONE RUBBER, HOT-OIL AND COOLANT RESISTANT |
| MS25438 Revision A:1964 | TERMINAL, LUG, CRIMP STYLE, RIGHT ANGLE TYPE, FOR ALUMINUM AIRCRAFT WIRE, CLASS 1 |
| MIL-I-7444 Revision D:1984 | INSULATION SLEEVING, ELECTRICAL FLEXIBLE |
| MIL-S-83519 Revision A:1984 | SPLICE, SHIELD TERMINATION, SOLDER STYLE, INSULATION, HEAT SHRINKABLE, ENVIRONMENT RESISTANT, GENERAL SPECIFICATION FOR |
| MIL-T-7928 Revision G:1976 | TERMINAL, LUG SPLICES, CONDUCTOR, CRIMP STYLE, COPPER, GENERAL SPECIFICATION FOR |
| MIL C 3655 : C | CONNECTOR, PLUG AND RECEPTACLE, ELECTRICAL [COAXIAL SERIES TWIN] AND ASSOCIATED FITTINGS, GENERAL SPECIFICATION FOR |
| MIL C 3607 : A | CONNECTOR, COAXIAL, RADIO FREQUENCY, SERIES PULSE GENERAL SPECIFICATION FOR |
| MIL-T-81714-11 Revision F:1988 | TERMINAL JUNCTION SYSTEM, TERMINAL JUNCTION BLOCKS, SECTIONAL, WIRE IN-LINE JUNCTIONS, SINGLE, SERIES 1 |
| NAS813:2012 | CAP, PROTECTIVE, ELECTRICAL CONNECTOR |
| NAS820:2012 | PLUG - PROTECTIVE, ELECTRICAL CONNECTOR |
| MIL C 49142 : 0 | CONNECTOR, PLUGS & RECEPTACLES, ELECTRICAL, TRIAXIAL,RADIO FREQUENCY, GENERAL SPECIFICATION FOR |
| MS3373 Revision C:1972 | STRIP, MOUNTING, NUT INSULATING, FOR MS27212 TERMINAL BOARD |
| MIL-C-6136 Revision A:1965 | Conduit: Electrical, Flexible, Shielded, Aluminum Alloy for Aircraft Installations (Use SAE-AS6136) |
| MIL-I-631 Revision D:1961 | INSULATION, ELECTRICAL, SYNTHETIC - RESIN COMPOSITION, NONRIGID |
| MIL-B-5087 Revision B:1964 | BONDING, ELECTRICAL AND LIGHTING PROTECTION, FOR AEROSPACE SYSTEMS |
| MS25171 Revision C:1959 | NIPPLE, ELECTRICAL TERMINAL (ASG) |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-STD-681 Revision F:2012 | IDENTIFICATION CODING AND APPLICATION OF HOOKUP AND LEAD WIRE |
| FED-STD-595 Revision C:2008 | COLORS USED IN GOVERNMENT PROCUREMENT |
| MS18029 Revision E:1971 | COVER ASSEMBLY ELECTRICAL FOR MS27212 TERMINAL BOARD ASSEMBLY |
| MIL-E-7080 Revision B:1962 | ELECTRIC EQUIPMENT, AIRCRAFT, SELECTION AND INSTALLATION OF |
| MS25435 Revision A:1964 | TERMINAL, LUG, CRIMP STYLE, STRAIGHT TYPE, FOR ALUMINUM AIRCRAFT WIRE CLASS 1 |
| MIL-F-7179 Revision G:1993 | FINISHES, COATINGS, AND SEALANTS FOR THE PROTECTION OF AEROSPACE WEAPONS SYSTEM |
| MS27488 Revision N:2008 | PLUG, END SEAL, ELECTRICAL CONNECTOR |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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